For a printed version of my book in color, please go to LuLu:
http://www.lulu.com/spotlight/flat_earth

For a free PDF version, click on one of these links:
https://www.slideshare.net/secret/vDreJQ21p75q5Q
or
https://www.flatearthresearch.com/wp-content/uploads/2019/12/covered16emergencylandingsprovingflatearth-191007025918.pdf?fbclid=IwAR3R5b0rNaFiRmEWoQBPw7PjIT6q0rXqGRAdztCiYU8kK8zb5j-WDsGBIWc

Free high-resolution Gleason’s Map:
https://www.dropbox.com/s/9lcp65memq7vyxd/hi%20res%20restored%20gleason%20map.png?dl=0

“It’s flat & motionless Folks! From the Pilot’s basic study guide; please read 1.1.2 & let that sink in! Every Pilot was taught this, but some still don’t get it, (I didn’t at first) & some just stay asleep & yes it does say ‘assumed’ but when does the theory become a spinning reality? Where is the next part B manual to apply Coriolis & curvature nonsense to any flight? Never…because it is a flat & stationary Earth we live & fly on. All flight planning & aerial navigation is based always on a flat motionless plane! Curvature or spin is never accounted for EVER 😱☯️😴”

http://www.aerostudents.com/courses/flight-dynamics/flightDynamicsFullVersion.pdf
Flat nonrotating earth

page 126:

“The nonlinear equations of motion used are six-degree-of-freedom equations

sith stationary atmosphere and flat, nonrotating earth”
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890007066.pdf

Determination of Angles of Attack and Sideslip from Radar Data and a Roll Stabilized Platform

NASA – March 1972 page 2:

“The method is limited, however, to application where a flat, nonrotating earth”

https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19720012071.pdf

An Aircraft Model for the AIAA Controls Design Challenge
NASA – 1991 – page 11:

“The nonlinear equations of motion used in this model are general six-degree-of-freedom equations representing the flight dynamics of a rigid aircraft flying in a stationary atmosphere over a flat non-rotating earth”
https://www.nasa.gov/centers/dryden/pdf/88248main_H-1777.pdf

Investigation of Aircraft Landing in Variable Wind Fields
NASA 1973 – page14 pdf or 6 on actual report:

a) The earth is flat and non-rotating.
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19790005472.pdf

A Mathematical Model of the CH-53 Helicopter

NASA – page 17:

“The helicopter equations of motion are given in body axes with rerpect to

a flat, nonrotating Earth.”

https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19810003557.pdf

Atmospheric Oscillations

Georgia Tech April 1965

Prepared for NASA

page 13:

A model frequently used is that of a flat, nonrotating earth.

https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19650015408.pdf

page 19:

These equations assume a rigid vehicle and a flat, nonrotating Earth.

https://www.nasa.gov/centers/dryden/pdf/88733main_H-2465.pdf

Flight Testing a VSTOL Aircraft

NASA 1988 – page 9 pdf or 4-5 on actual doc:

“For aircraft problems, the state and measurement models together represent the kinematics of a rigid body for describing motion over a flat, nonrotating Earth…”

https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19880014378.pdf

Time to Climb

page2:

“In our minimum time-to-climb problem, the aircraft is modeled as a point mass and the flight trajectory is strictly

confined in a vertical plane on a non-rotating, flat earth.

https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20060053337.pdf?